A three-dimensional numerical simulation of a combustion chamber with a continuous rotating detonation wave was studied. A nozzle-type main system feeding was located at the end part of the chamber, and an additional feeding from the inner and outer walls of the annular channel was considered. A hydrogen-oxygen mixture was considered as a fuel. A detailed kinetic mechanism by Z. Hong (2010) consisting of 20 reactions with 9 components was used to simulate chemical processes. Various relations of the fuel were considered: lean mixture [H₂]:[O₂] = 1:1, stoichiometric mixture [H₂]:[O₂] = 2:1, and rich mixture [H₂]:[O₂] = 3:1. Besides, either the same mixture, or additional oxygen, or air was supplied from the side-wall feeding system. For all the considered feeding options, a detonation mode was obtained, and the traction characteristics were calculated.

研究了连续旋转爆震波燃烧室的三维数值模拟。喷嘴式主系统进料位于腔室端部，并考虑从环形通道的内外壁进行额外进料。氢氧混合物被认为是一种燃料。Z. Hong (2010) 的详细动力学机制由 9 个组分的 20 个反应组成，用于模拟化学过程。考虑了燃料的各种关系：稀混合气[H ₂ ]:[O ₂ ] = 1:1，化学计量混合气[H ₂ ]:[O ₂ ] = 2:1，富混合气[H ₂ ]:[O ₂] = 3:1。此外，从侧壁进料系统供应相同的混合物或额外的氧气或空气。对于所有考虑的进料选项，获得了爆轰模式，并计算了牵引特性。